Method for operating a powertrain system to control engine stabilization

ABSTRACT

An engine is selectively operative in one of a plurality of engine states to transfer torque to an input member of a hybrid transmission. The hybrid transmission is operative to transfer torque between the input member and a torque machine and an output member to generate an output torque in response to an operator torque request. A method for controlling the engine includes monitoring the operator torque request, determining operating power costs associated with a plurality of candidate engine states in response to the operator torque request, determining transition costs for transitioning the engine from a present engine state to each of the candidate engine states, determining stabilization costs for operating the engine in the present engine state and subsequently operating the engine in each of the candidate engine states, and selecting a preferred engine state based upon the operating power costs, the transition costs, and the stabilization costs for the plurality of engine states.

CROSS REFERENCE TO RELATED APPLICATION

This application claims the benefit of U.S. Provisional Application No. 60/985,410 filed on Nov. 5, 2007 which is hereby incorporated herein by reference.

TECHNICAL FIELD

This disclosure is related to controlling engine stabilization within a powertrain system.

BACKGROUND

The statements in this section merely provide background information related to the present disclosure and may not constitute prior art.

Known powertrain architectures include torque-generative devices, including internal combustion engines and torque machines that transmit torque through a transmission device to an output member. One exemplary powertrain includes a two-mode, compound-split, electromechanical transmission which utilizes an input member for receiving motive torque from a prime mover power source, preferably an internal combustion engine, and an output member. The output member can be operatively connected to a driveline for a motor vehicle for transmitting tractive torque thereto. Electric machines, operative as motors or generators, generate a torque input to the transmission, independently of a torque input from the internal combustion engine. The electric machines may transform vehicle kinetic energy, transmitted through the vehicle driveline, to electrical energy that is storable in an electrical energy storage device. A control system monitors various inputs from the vehicle and the operator and provides operational control of the powertrain, including controlling transmission operating state and gear shifting, controlling the torque-generative devices, and regulating the electrical power interchange among the electrical energy storage device and the electric machines to manage outputs of the transmission, including torque and rotational speed.

SUMMARY

An engine is selectively operative in one of a plurality of engine states to transfer torque to an input member of a hybrid transmission. The hybrid transmission is operative to transfer torque between the input member and a torque machine and an output member to generate an output torque in response to an operator torque request. A method for controlling the engine includes monitoring the operator torque request, determining operating power costs associated with a plurality of candidate engine states in response to the operator torque request, determining transition costs for transitioning the engine from a present engine state to each of the candidate engine states, determining stabilization costs for operating the engine in the present engine state and subsequently operating the engine in each of the candidate engine states, and selecting a preferred engine state based upon the operating power costs, the transition costs, and the stabilization costs for the plurality of engine states.

BRIEF DESCRIPTION OF THE DRAWINGS

One or more embodiments will now be described, by way of example, with reference to the accompanying drawings, in which:

FIG. 1 is a schematic diagram of an exemplary powertrain, in accordance with the present disclosure;

FIG. 2 is a schematic diagram of an exemplary architecture for a control system and powertrain, in accordance with the present disclosure;

FIGS. 3 and 4 are schematic flow diagrams of a control system architecture for controlling and managing torque in a powertrain system, in accordance with the present disclosure; and

FIG. 5 is a schematic flow diagram, in accordance with the present disclosure.

DETAILED DESCRIPTION

Referring now to the drawings, wherein the showings are for the purpose of illustrating certain exemplary embodiments only and not for the purpose of limiting the same, FIGS. 1 and 2 depict an exemplary mechanical hybrid powertrain. The exemplary hybrid powertrain in accordance with the present disclosure is depicted in FIG. 1, comprising a two-mode, compound-split, electromechanical hybrid transmission 10 operatively connected to an engine 14 and first and second electric machines (‘MG-A’) 56 and (‘MG-B’) 72. The engine 14 and first and second electric machines 56 and 72 each generate power which can be transferred to the transmission 10. The power generated by the engine 14 and the first and second electric machines 56 and 72 and transferred to the transmission 10 is described in terms of input and motor torques, referred to herein as T_(I), T_(A), and T_(B) respectively, and speed, referred to herein as N_(I), N_(A), and N_(B), respectively.

The exemplary engine 14 comprises a multi-cylinder internal combustion engine selectively operative in several states to transfer torque to the transmission 10 via an input shaft 12, and can be either a spark-ignition or a compression-ignition engine. The engine 14 includes a crankshaft (not shown) operatively coupled to the input shaft 12 of the transmission 10. A rotational speed sensor 11 monitors rotational speed of the input shaft 12. Power output from the engine 14, comprising rotational speed and engine torque, can differ from the input speed N_(I) and the input torque T_(I) to the transmission 10 due to placement of torque-consuming components on the input shaft 12 between the engine 14 and the transmission 10, e.g., a hydraulic pump (not shown) and/or a torque management device (not shown).

The exemplary transmission 10 comprises three planetary-gear sets 24, 26 and 28, and four selectively engageable torque-transferring devices, i.e., clutches C1 70, C2 62, C3 73, and C4 75. As used herein, clutches refer to any type of friction torque transfer device including single or compound plate clutches or packs, band clutches, and brakes, for example. A hydraulic control circuit 42, preferably controlled by a transmission control module (hereafter ‘TCM’) 17, is operative to control clutch states. Clutches C2 62 and C4 75 preferably comprise hydraulically-applied rotating friction clutches. Clutches C1 70 and C3 73 preferably comprise hydraulically-controlled stationary devices that can be selectively grounded to a transmission case 68. Each of the clutches C1 70, C2 62, C3 73, and C4 75 is preferably hydraulically applied, selectively receiving pressurized hydraulic fluid via the hydraulic control circuit 42.

The first and second electric machines 56 and 72 preferably comprise three-phase AC machines, each including a stator (not shown) and a rotor (not shown), and respective resolvers 80 and 82. The motor stator for each machine is grounded to an outer portion of the transmission case 68, and includes a stator core with coiled electrical windings extending therefrom. The rotor for the first electric machine 56 is supported on a hub plate gear that is operatively attached to shaft 60 via the second planetary gear set 26. The rotor for the second electric machine 72 is fixedly attached to a sleeve shaft hub 66.

Each of the resolvers 80 and 82 preferably comprises a variable reluctance device including a resolver stator (not shown) and a resolver rotor (not shown). The resolvers 80 and 82 are appropriately positioned and assembled on respective ones of the first and second electric machines 56 and 72. Stators of respective ones of the resolvers 80 and 82 are operatively connected to one of the stators for the first and second electric machines 56 and 72. The resolver rotors are operatively connected to the rotor for the corresponding first and second electric machines 56 and 72. Each of the resolvers 80 and 82 is signally and operatively connected to a transmission power inverter control module (hereafter ‘TPIM’) 19, and each senses and monitors rotational position of the resolver rotor relative to the resolver stator, thus monitoring rotational position of respective ones of first and second electric machines 56 and 72. Additionally, the signals output from the resolvers 80 and 82 are interpreted to provide the rotational speeds for first and second electric machines 56 and 72, i.e., N_(A) and N_(B), respectively.

The transmission 10 includes an output member 64, e.g. a shaft, which is operably connected to a driveline 90 for a vehicle (not shown), to provide output power to the driveline 90 that is transferred to vehicle wheels 93, one of which is shown in FIG. 1. The output power at the output member 64 is characterized in terms of an output rotational speed N_(O) and an output torque T_(O). A transmission output speed sensor 84 monitors rotational speed and rotational direction of the output member 64. Each of the vehicle wheels 93 is preferably equipped with a sensor 94 adapted to monitor wheel speed, the output of which is monitored by a control module of a distributed control module system described with respect to FIG. 2, to determine vehicle speed, and absolute and relative wheel speeds for braking control, traction control, and vehicle acceleration management.

The input torque from the engine 14 and the motor torques from the first and second electric machines 56 and 72 (T_(I), T_(A), and T_(B) respectively) are generated as a result of energy conversion from fuel or electrical potential stored in an electrical energy storage device (hereafter ‘ESD’) 74. The ESD 74 is high voltage DC-coupled to the TPIM 19 via DC transfer conductors 27. The transfer conductors 27 include a contactor switch 38. When the contactor switch 38 is closed, under normal operation, electric current can flow between the ESD 74 and the TPIM 19. When the contactor switch 38 is opened electric current flow between the ESD 74 and the TPIM 19 is interrupted. The TPIM 19 transmits electrical power to and from the first electric machine 56 by transfer conductors 29, and the TPIM 19 similarly transmits electrical power to and from the second electric machine 72 by transfer conductors 31 to meet the torque commands for the first and second electric machines 56 and 72 in response to the motor torques T_(A) and T_(B) . Electrical current is transmitted to and from the ESD 74 in accordance with whether the ESD 74 is being charged or discharged.

The TPIM 19 includes the pair of power inverters (not shown) and respective motor control modules (not shown) configured to receive the torque commands and control inverter states therefrom for providing motor drive or regeneration functionality to meet the commanded motor torques T_(A) and T_(B). The power inverters comprise known complementary three-phase power electronics devices, and each includes a plurality of insulated gate bipolar transistors (not shown) for converting DC power from the ESD 74 to AC power for powering respective ones of the first and second electric machines 56 and 72, by switching at high frequencies. The insulated gate bipolar transistors form a switch mode power supply configured to receive control commands. There is typically one pair of insulated gate bipolar transistors for each phase of each of the three-phase electric machines. States of the insulated gate bipolar transistors are controlled to provide motor drive mechanical power generation or electric power regeneration functionality. The three-phase inverters receive or supply DC electric power via DC transfer conductors 27 and transform it to or from three-phase AC power, which is conducted to or from the first and second electric machines 56 and 72 for operation as motors or generators via transfer conductors 29 and 31 respectively.

FIG. 2 is a schematic block diagram of the distributed control module system. The elements described hereinafter comprise a subset of an overall vehicle control architecture, and provide coordinated system control of the exemplary hybrid powertrain described in FIG. 1. The distributed control module system synthesizes pertinent information and inputs, and executes algorithms to control various actuators to meet control objectives, including objectives related to fuel economy, emissions, performance, drivability, and protection of hardware, including batteries of ESD 74 and the first and second electric machines 56 and 72. The distributed control module system includes an engine control module (hereafter ‘ECM’) 23, the TCM 17, a battery pack control module (hereafter ‘BPCM’) 21, and the TPIM 19. A hybrid control module (hereafter ‘HCP’) 5 provides supervisory control and coordination of the ECM 23, the TCM 17, the BPCM 21, and the TPIM 19. A user interface (‘UI’) 13 is operatively connected to a plurality of devices through which a vehicle operator controls or directs operation of the electromechanical hybrid powertrain. The devices include an accelerator pedal 113 (‘AP’), an operator brake pedal 112 (‘BP’), a transmission gear selector 114 (‘PRNDL’), and a vehicle speed cruise control (not shown). The transmission gear selector 114 may have a discrete number of operator-selectable positions, including the rotational direction of the output member 64 to enable one of a forward and a reverse direction.

The aforementioned control modules communicate with other control modules, sensors, and actuators via a local area network (hereafter ‘LAN’) bus 6. The LAN bus 6 allows for structured communication of states of operating parameters and actuator command signals between the various control modules. The specific communication protocol utilized is application-specific. The LAN bus 6 and appropriate protocols provide for robust messaging and multi-control module interfacing between the aforementioned control modules, and other control modules providing functionality including e.g., antilock braking, traction control, and vehicle destabilization. Multiple communications buses may be used to improve communications speed and provide some level of signal redundancy and integrity. Communication between individual control modules can also be effected using a direct link, e.g., a serial peripheral interface (‘SPI’) bus (not shown).

The HCP 5 provides supervisory control of the hybrid powertrain, serving to coordinate operation of the ECM 23, TCM 17, TPIM 19, and BPCM 21. Based upon various input signals from the user interface 13 and the hybrid powertrain, including the ESD 74, the HCP 5 determines an operator torque request, an output torque command, an engine input torque command, clutch torque(s) for the applied torque-transfer clutches C1 70, C2 62, C3 73, C4 75 of the transmission 10, and the motor torques T_(A) and T_(B) for the first and second electric machines 56 and 72. The TCM 17 is operatively connected to the hydraulic control circuit 42 and provides various functions including monitoring various pressure sensing devices (not shown) and generating and communicating control signals to various solenoids (not shown) thereby controlling pressure switches and control valves contained within the hydraulic control circuit 42.

The ECM 23 is operatively connected to the engine 14, and functions to acquire data from sensors and control actuators of the engine 14 over a plurality of discrete lines, shown for simplicity as an aggregate bi-directional interface cable 35. The ECM 23 receives the engine input torque command from the HCP 5. The ECM 23 determines the present engine input torque, T_(I), provided to the transmission 10 at that point in time based upon monitored engine speed and load, which is communicated to the HCP 5. The ECM 23 monitors input from the rotational speed sensor 11 to determine the engine input speed to the input shaft 12, which translates to the transmission input speed, N_(I). The ECM 23 monitors inputs from sensors (not shown) to determine states of other engine operating parameters including, e.g., a manifold pressure, engine coolant temperature, ambient air temperature, and ambient pressure. The engine load can be determined, for example, from the manifold pressure, or alternatively, from monitoring operator input to the accelerator pedal 113. The ECM 23 generates and communicates command signals to control engine actuators, including, e.g., fuel injectors, ignition modules, and throttle control modules, none of which are shown.

The TCM 17 is operatively connected to the transmission 10 and monitors inputs from sensors (not shown) to determine states of transmission operating parameters. The TCM 17 generates and communicates command signals to control the transmission 10, including controlling the hydraulic control circuit 42. Inputs from the TCM 17 to the HCP 5 include estimated clutch torques for each of the clutches, i.e., C1 70, C2 62, C3 73, and C4 75, and rotational output speed, N_(O), of the output member 64. Other actuators and sensors may be used to provide additional information from the TCM 17 to the HCP 5 for control purposes. The TCM 17 monitors inputs from pressure switches (not shown) and selectively actuates pressure control solenoids (not shown) and shift solenoids (not shown) of the hydraulic control circuit 42 to selectively actuate the various clutches C1 70, C2 62, C3 73, and C4 75 to achieve various transmission operating range states, as described hereinbelow.

The BPCM 21 is signally connected to sensors (not shown) to monitor the ESD 74, including states of electrical current and voltage parameters, to provide information indicative of parametric states of the batteries of the ESD 74 to the HCP 5. The parametric states of the batteries preferably include battery state-of-charge, battery voltage, battery temperature, and available battery power, referred to as a range P_(BAT) _(—) _(MIN) to P_(BAT) _(—) _(MAX).

A brake control module (hereafter ‘BrCM’) 22 is operatively connected to friction brakes (not shown) on each of the vehicle wheels 93. The BrCM 22 monitors the operator input to the brake pedal 112 and generates control signals to control the friction brakes and sends a control signal to the HCP 5 to operate the first and second electric machines 56 and 72 based thereon.

Each of the control modules ECM 23, TCM 17, TPIM 19, BPCM 21, and BrCM 22 is preferably a general-purpose digital computer comprising a microprocessor or central processing unit, storage mediums comprising read only memory (‘ROM’), random access memory (‘RAM’), electrically programmable read only memory (‘EPROM’), a high speed clock, analog to digital (‘A/D’) and digital to analog (‘D/A’) circuitry, and input/output circuitry and devices (‘I/O’) and appropriate signal conditioning and buffer circuitry. Each of the control modules has a set of control algorithms, comprising resident program instructions and calibrations stored in one of the storage mediums and executed to provide the respective functions of each computer. Information transfer between the control modules is preferably accomplished using the LAN bus 6 and SPI buses. The control algorithms are executed during preset loop cycles such that each algorithm is executed at least once each loop cycle. Algorithms stored in the non-volatile memory devices are executed by one of the central processing units to monitor inputs from the sensing devices and execute control and diagnostic routines to control operation of the actuators, using preset calibrations. Loop cycles are executed at regular intervals, for example each 3.125, 6.25, 12.5, 25 and 100 milliseconds during ongoing operation of the hybrid powertrain. Alternatively, algorithms may be executed in response to the occurrence of an event.

The exemplary hybrid powertrain selectively operates in one of several operating range states that can be described in terms of an engine state comprising one of an engine-on state (‘ON’) and an engine-off state (‘OFF’), and a transmission state comprising a plurality of fixed gears and continuously variable operating modes, described with reference to Table 1, below.

TABLE 1 Engine Transmission Operating Applied Description State Range State Clutches M1_Eng_Off OFF EVT Mode 1 C1 70 M1_Eng_On ON EVT Mode 1 C1 70 G1 ON Fixed Gear Ratio 1 C1 70 C4 75 G2 ON Fixed Gear Ratio 2 C1 70 C2 62 M2_Eng_Off OFF EVT Mode 2 C2 62 M2_Eng_On ON EVT Mode 2 C2 62 G3 ON Fixed Gear Ratio 3 C2 62 C4 75 G4 ON Fixed Gear Ratio 4 C2 62 C3 73

Each of the transmission operating range states is described in the table and indicates which of the specific clutches C1 70, C2 62, C3 73, and C4 75 are applied for each of the operating range states. A first continuously variable mode, i.e., EVT Mode 1, or M1, is selected by applying clutch C1 70 only in order to “ground” the outer gear member of the third planetary gear set 28. The engine state can be one of ON (‘M1_Eng_On’) or OFF (‘M1_Eng_Off’). A second continuously variable mode, i.e., EVT Mode 2, or M2, is selected by applying clutch C2 62 only to connect the shaft 60 to the carrier of the third planetary gear set 28. The engine state can be one of ON (‘M2_Eng_On’) or OFF (‘M2_Eng_Off’). For purposes of this description, when the engine state is OFF, the engine input speed is equal to zero revolutions per minute (‘RPM’), i.e., the engine crankshaft is not rotating. A fixed gear operation provides a fixed ratio operation of input-to-output speed of the transmission 10, i.e., N_(I)/N_(O). A first fixed gear operation (‘G1’) is selected by applying clutches C1 70 and C4 75. A second fixed gear operation (‘G2’) is selected by applying clutches C1 70 and C2 62. A third fixed gear operation (‘G3’) is selected by applying clutches C2 62 and C4 75. A fourth fixed gear operation (‘G4’) is selected by applying clutches C2 62 and C3 73. The fixed ratio operation of input-to-output speed increases with increased fixed gear operation due to decreased gear ratios in the planetary gears 24, 26, and 28. The rotational speeds of the first and second electric machines 56 and 72, N_(A) and N_(B) respectively, are dependent on internal rotation of the mechanism as defined by the clutching and are proportional to the input speed measured at the input shaft 12.

In response to operator input via the accelerator pedal 113 and brake pedal 112 as captured by the user interface 13, the HCP 5 and one or more of the other control modules determine torque commands to control the torque generative devices comprising the engine 14 and first and second electric machines 56 and 72 to meet the operator torque request at the output member 64 and transferred to the driveline 90. Based upon input signals from the user interface 13 and the hybrid powertrain including the ESD 74, the HCP 5 determines the operator torque request, a commanded output torque from the transmission 10 to the driveline 90, an input torque from the engine 14, clutch torques for the torque-transfer clutches C1 70, C2 62, C3 73, C4 75 of the transmission 10; and the motor torques for the first and second electric machines 56 and 72, respectively, as is described hereinbelow.

Final vehicle acceleration can be affected by other factors including, e.g., road load, road grade, and vehicle mass. The operating range state is determined for the transmission 10 based upon a variety of operating characteristics of the hybrid powertrain. This includes the operator torque request communicated through the accelerator pedal 113 and brake pedal 112 to the user interface 13 as previously described. The operating range state may be predicated on a hybrid powertrain torque demand caused by a command to operate the first and second electric machines 56 and 72 in an electrical energy generating mode or in a torque generating mode. The operating range state can be determined by an optimization algorithm or routine which determines optimum system efficiency based upon operator demand for power, battery state of charge, and energy efficiencies of the engine 14 and the first and second electric machines 56 and 72. The control system manages torque inputs from the engine 14 and the first and second electric machines 56 and 72 based upon an outcome of the executed optimization routine, and system efficiencies are optimized thereby, to manage fuel economy and battery charging. Furthermore, operation can be determined based upon a fault in a component or system. The HCP 5 monitors the torque-generative devices, and determines the power output from the transmission 10 required in response to the desired output torque at output member 64 to meet the operator torque request. As should be apparent from the description above, the ESD 74 and the first and second electric machines 56 and 72 are electrically-operatively coupled for power flow therebetween. Furthermore, the engine 14, the first and second electric machines 56 and 72, and the electromechanical transmission 10 are mechanically-operatively coupled to transfer power therebetween to generate a power flow to the output member 64.

FIG. 3 shows a control system architecture for controlling and managing torque and power flow in a powertrain system having multiple torque generative devices, described hereinbelow with reference to the hybrid powertrain system shown in FIGS. 1 and 2, and residing in the aforementioned control modules in the form of executable algorithms and calibrations. The control system architecture can be applied to any powertrain system having multiple torque generative devices, including, e.g., a hybrid powertrain system having a single electric machine, a hybrid powertrain system having multiple electric machines, and non-hybrid powertrain systems.

The control system architecture of FIG. 3 depicts a flow of pertinent signals through the control modules. In operation, the operator inputs to the accelerator pedal 113 and the brake pedal 112 are monitored to determine the operator torque request (‘To_req’). Operation of the engine 14 and the transmission 10 are monitored to determine the input speed (‘Ni’) and the output speed (‘No’). A strategic optimization control scheme (‘Strategic Control’) 310 determines a preferred input speed (‘Ni_Des’) and a preferred engine state and transmission operating range state (‘Hybrid Range State Des’) based upon the output speed and the operator torque request, and optimized based upon other operating parameters of the hybrid powertrain, including battery power limits and response limits of the engine 14, the transmission 10, and the first and second electric machines 56 and 72. The strategic optimization control scheme 310 is preferably executed by the HCP 5 during each 100 ms loop cycle and each 25 ms loop cycle.

The outputs of the strategic optimization control scheme 310 are used in a shift execution and engine start/stop control scheme (‘Shift Execution and Engine Start/Stop’) 320 to command changes in the transmission operation (‘Transmission Commands’) including changing the operating range state. This includes commanding execution of a change in the operating range state if the preferred operating range state is different from the present operating range state by commanding changes in application of one or more of the clutches C1 70, C2 62, C3 73, and C4 75 and other transmission commands. The present operating range state (‘Hybrid Range State Actual’) and an input speed profile (‘Ni_Prof’) can be determined. The input speed profile is an estimate of an upcoming input speed and preferably comprises a scalar parametric value that is a targeted input speed for the forthcoming loop cycle. The engine operating commands and the operator torque request are based upon the input speed profile during a transition in the operating range state of the transmission.

A tactical control scheme (‘Tactical Control and Operation’) 330 is repeatedly executed during one of the control loop cycles to determine engine commands (‘Engine Commands’) for operating the engine, including a preferred input torque from the engine 14 to the transmission 10 based upon the output speed, the input speed, and the operator torque request and the present operating range state for the transmission. The engine commands also include engine states including one of an all-cylinder operating state and a cylinder deactivation operating state, wherein a portion of the engine cylinders are deactivated and unfueled, and engine states including one of a fueled state and a fuel cutoff state, wherein fuel is cutoff from all-cylinders of the engine 14.

A clutch torque (‘Tcl’) for each clutch is estimated in the TCM 17, including the presently applied clutches and the non-applied clutches, and a present engine input torque (‘Ti’) reacting with the input member 12 is determined in the ECM 23. An output and motor torque determination scheme (‘Output and Motor Torque Determination’) 340 is executed to determine the preferred output torque from the powertrain (‘To_cmd’), which includes motor torque commands (‘T_(A)’, ‘T_(B)’) for controlling the first and second electric machines 56 and 72 in this embodiment. The preferred output torque is based upon the estimated clutch torque(s) for each of the clutches, the present input torque from the engine 14, the present operating range state, the input speed, the operator torque request, and the input speed profile. The first and second electric machines 56 and 72 are controlled through the TPIM 19 to meet the preferred motor torque commands based upon the preferred output torque. The output and motor torque determination scheme 340 includes algorithmic code which is regularly executed during the 6.25 ms and 12.5 ms loop cycles to determine the preferred motor torque commands.

FIG. 4 details signal flow in the tactical control scheme (‘Tactical Control and Operation’) 330 for controlling operation of the engine 14, described with reference to the hybrid powertrain system of FIGS. 1 and 2 and the control system architecture of FIGS. 3 and 4. The tactical control scheme 330 includes a tactical optimization control path 350 and a system constraints control path 360 which are preferably executed concurrently. The outputs of the tactical optimization control path 350 are input to an engine state control scheme 370. The outputs of the engine state control scheme 370 and the system constraints control path 360 are input to an engine response type determination scheme (‘Engine Response Type Determination’) 380 for controlling the engine state, the immediate engine torque request, the predicted engine torque request, and the engine response type.

The input from the engine 14 can be described in terms of an engine operating point including engine speed and engine torque which can be converted into the input speed and input torque which react with the input member from the transmission 10. When the engine 14 comprises a spark-ignition engine, a change in the engine operating point can be effected by changing mass of intake air to the engine 14, by controlling position of an engine throttle (not shown) utilizing an electronic throttle control system (not shown), including opening the engine throttle to increase engine torque and closing the engine throttle to decrease engine torque. Changes in the engine operating point can be effected by adjusting ignition timing, including retarding spark timing from a mean-best-torque spark timing to decrease engine torque. When the engine 14 comprises a compression-ignition engine, the engine operating point is controlled by controlling the mass of injected fuel and adjusted by retarding injection timing from a mean-best-torque injection timing to decrease the engine torque. The engine operating point can be changed to effect a change in the input torque by changing the engine state between the engine-off state and the engine-on state, by controlling the engine state between the all-cylinder state and the cylinder deactivation state, and, by controlling the engine state between the engine-fueled state and the fuel cutoff state wherein the engine is rotating and unfueled to effect engine braking.

In operation, operator inputs to the accelerator pedal 113 and to the brake pedal 112 are monitored to determine the operator torque request. Present speeds of the output member 64 and the input member 12, i.e., No and Ni, are determined. A present operating range state of the transmission 14 and present engine states are determined. Maximum and minimum electric power tactical control power constraints of the electric energy storage device 74 are determined.

The operator inputs to the accelerator pedal 113 and the brake pedal 112 comprise individually determinable operator torque request inputs including an immediate accelerator output torque request (‘Output Torque Request Accel Immed’), a predicted accelerator output torque request (‘Output Torque Request Accel Prdtd’), an immediate brake output torque request (‘Output Torque Request Brake Immed’), a predicted brake output torque request (‘Output Torque Request Brake Prdtd’) and an axle torque response type (‘Axle Torque Response Type’). As used herein, the term ‘accelerator’ refers to an operator request for forward propulsion preferably resulting in increasing vehicle speed over the present vehicle speed, when the operator selected position of the transmission gear selector 114 commands operation of the vehicle in the forward direction, and a similar reverse propulsion response when the vehicle operation is commanded in the reverse direction. The terms ‘deceleration’ and ‘brake’ refer to an operator request preferably resulting in decreasing vehicle speed from the present vehicle speed. The immediate accelerator output torque request, the predicted accelerator output torque request, the immediate brake output torque request, the predicted brake output torque request, and the axle torque response type are individual inputs to the control system shown in FIG. 3.

The immediate accelerator output torque request comprises an immediate torque request determined based upon the operator input to the accelerator pedal 113. The control system controls the output torque from the hybrid powertrain system in response to the immediate accelerator output torque request to cause positive acceleration of the vehicle. The immediate brake output torque request comprises an immediate braking request determined based upon the operator input to the brake pedal 112. The control system controls the output torque from the hybrid powertrain system in response to the immediate brake output torque request to cause deceleration, or negative acceleration, of the vehicle. Vehicle deceleration effected by control of the output torque from the hybrid powertrain system is combined with vehicle deceleration effected by a vehicle braking system (not shown) to decelerate the vehicle to achieve the immediate braking request.

The immediate accelerator output torque request is determined based upon a presently occurring operator input to the accelerator pedal 113, and comprises a request to generate an immediate output torque at the output member 64 preferably to accelerate the vehicle. The immediate accelerator output torque request is unshaped, but can be shaped by events that affect vehicle operation outside the powertrain control. Such events include vehicle level interruptions in the powertrain control for antilock braking, traction control and vehicle destabilization control, which can be used to unshape or rate-limit the immediate accelerator output torque request.

The predicted accelerator output torque request is determined based upon the operator input to the accelerator pedal 113 and comprises an optimum or preferred output torque at the output member 64. The predicted accelerator output torque request is preferably equal to the immediate accelerator output torque request during normal operating conditions, e.g., when any one of antilock braking, traction control, or vehicle destabilization is not being commanded. When any one of antilock braking, traction control or vehicle destabilization is being commanded the predicted accelerator output torque request remains the preferred output torque with the immediate accelerator output torque request being decreased in response to output torque commands related to the antilock braking, traction control, or vehicle destabilization control.

Blended brake torque includes a combination of the friction braking torque generated at the wheels 93 and the output torque generated at the output member 64 which reacts with the driveline 90 to decelerate the vehicle in response to the operator input to the brake pedal 112.

The immediate brake output torque request is determined based upon a presently occurring operator input to the brake pedal 112, and comprises a request to generate an immediate output torque at the output member 64 to effect a reactive torque with the driveline 90 which preferably decelerates the vehicle. The immediate brake output torque request is determined based upon the operator input to the brake pedal 112 and the control signal to control the friction brakes to generate friction braking torque.

The predicted brake output torque request comprises an optimum or preferred brake output torque at the output member 64 in response to an operator input to the brake pedal 112 subject to a maximum brake output torque generated at the output member 64 allowable regardless of the operator input to the brake pedal 112. In one embodiment the maximum brake output torque generated at the output member 64 is limited to −0.2 g. The predicted brake output torque request can be phased out to zero when vehicle speed approaches zero regardless of the operator input to the brake pedal 112. As desired by a user, there can be operating conditions under which the predicted brake output torque request is set to zero, e.g., when the operator setting to the transmission gear selector 114 is set to a reverse gear, and when a transfer case (not shown) is set to a four-wheel drive low range. The operating conditions whereat the predicted brake output torque request is set to zero are those in which blended braking is not preferred due to vehicle operating factors.

The axle torque response type comprises an input state for shaping and rate-limiting the output torque response through the first and second electric machines 56 and 72. The input state for the axle torque response type can be an active state, preferably comprising one of a pleasability limited state a maximum range state, and an inactive state. When the commanded axle torque response type is the active state, the output torque command is the immediate output torque. Preferably the torque response for this response type is as fast as possible.

The tactical optimization control path 350 acts on substantially steady-state inputs to select a preferred engine state and determine a preferred input torque from the engine 14 to the transmission 10. The inputs originate in the shift execution and engine start/stop control scheme 320. The tactical optimization control path 350 includes an optimization scheme (‘Tactical Optimization’) 354 to determine preferred input torques for operating the engine 14 in the all-cylinder state (‘Input Torque Full’), in the cylinder deactivation state (‘Input Torque Deac’), the all-cylinder state with fuel cutoff (‘Input Torque Full FCO’), in the cylinder deactivation state with fuel cutoff (‘Input Torque Deac FCO’), and a preferred engine state (‘Engine State’). Inputs to the optimization scheme 354 include a lead operating range state of the transmission 10 (‘Lead Hybrid Range State’) a lead predicted input acceleration profile (‘Lead Input Acceleration Profile Predicted’), a predicted range of clutch reactive torques (‘Predicted Clutch Reactive Torque Min/Max’) across each applied clutch in the lead operating range state, predicted electric power limits (‘Predicted Battery Power Limits’), a predicted accelerator output torque request (‘Output Torque Request Accel Prdtd’) and a predicted braking output torque request (‘Output Torque Request Brake Prdtd’). The predicted output torque requests for acceleration and braking are combined and shaped with the axle torque response type through a predicted output torque shaping filter 352 to yield a net predicted output torque (‘To Net Prdtd’) and a predicted accelerator output torque (‘To Accel Prdtd’), which are inputs to the optimization scheme 354. The lead operating range state of the transmission 10 comprises a time-shifted lead of the operating range state of the transmission 10 to accommodate a response time lag between a commanded change in the operating range state and the present operating range state. Thus the lead operating range state of the transmission 10 is the commanded operating range state. The lead predicted input acceleration profile comprises a time-shifted lead of the predicted input acceleration profile of the input member 12 to accommodate a response time lag between a commanded change in the predicted input acceleration profile and a measured change in the predicted input acceleration profile. Thus the lead predicted input acceleration profile is the predicted input acceleration profile of the input member 12 occurring after the time shift. The parameters designated as ‘lead’ are used to accommodate concurrent transfer of torque through the powertrain converging at the common output member 64 using devices having varying response times. Specifically, the engine 14 can have a response time of an order of magnitude of 300-600 ms, and each of the torque transfer clutches C1 70, C2 62, C3 73, and C4 75 can have response times of an order of magnitude of 150-300 ms, and the first and second electric machines 56 and 72 can have response time of an order of magnitude of 10 ms.

The optimization scheme 354 determines costs for operating the engine 14 in the engine states, which comprise operating the engine in the fueled, all-cylinder state (‘P_(COST FULL FUEL)’), operating the engine in the fuel cutoff, all-cylinder state (‘P_(COST FULL FCO)’), operating the engine in the fueled, cylinder deactivation state (‘P_(COST DEAC FUEL)’), and operating the engine in the fuel cutoff, cylinder deactivation state (‘P_(COST DEAC FCO)’). The aforementioned costs for operating the engine 14 are input to a stabilization analysis scheme (‘Stabilization and Arbitration’) 356 along with the present engine state (‘Actual Engine State’) and allowable or permissible engine states (‘Engine State Allowed’) to select one of the engine states as the preferred engine state (‘Preferred Engine State’).

The preferred input torques for operating the engine 14 in the all-cylinder state and in the cylinder deactivation state with and without fuel cutoff are input to an engine torque conversion calculator 355 and converted to preferred engine torques in the all-cylinder state and in the cylinder deactivation state (‘Optimal Engine Torque Full’) and (‘Optimal Engine Torque Deac’) and with fuel cutoff in the all-cylinder state and in the cylinder deactivation state (‘Engine Torque Full FCO’) and (‘Engine Torque Deac FCO’) respectively, by taking into account parasitic and other loads introduced between the engine 14 and the transmission 10. The preferred engine torques for operation in the all-cylinder state and in the cylinder deactivation state and the preferred engine state comprise inputs to the engine state control scheme 370.

The costs for operating the engine 14 include operating costs which are determined based upon factors that include vehicle driveability, fuel economy, emissions, and battery usage. Costs are assigned and associated with fuel and electrical power consumption and are associated with a specific operating points of the hybrid powertrain. Lower operating costs can be associated with lower fuel consumption at high conversion efficiencies, lower battery power usage, and lower emissions for each engine speed/load operating point, and take into account the present operating state of the engine 14.

The preferred engine state and the preferred engine torques in the all-cylinder state and in the cylinder deactivation state are input to the engine state control scheme 370, which includes an engine state machine (‘Engine State Machine’) 372. The engine state machine 372 determines a target engine torque (‘Target Engine Torque’) and an engine state (‘Engine State’) based upon the preferred engine torques and the preferred engine state. The target engine torque and the engine state are input to a transition filter 374 which monitors any commanded transition in the engine state and filters the target engine torque to provide a filtered target engine torque (‘Filtered Target Engine Torque’). The engine state machine 372 outputs a command that indicates selection of one of the cylinder deactivation state and the all-cylinder state (‘DEAC Selected’) and indicates selection of one of the engine-fueled state and the deceleration fuel cutoff state (‘FCO Selected’).

The selection of one of the cylinder deactivation state and the all-cylinder state and the selection of one of the engine-fueled state and the deceleration fuel cutoff state, the filtered target engine torque, and the minimum and maximum engine torques are input to the engine response type determination scheme 380.

The system constraints control path 360 determines the constraints on the input torque, comprising minimum and maximum input torques (‘Input Torque Hybrid Minimum’ and ‘Input Torque Hybrid Maximum’) that can be reacted by the transmission 10. The minimum and maximum input torques are determined based upon constraints to the transmission 10, the first and second electric machines 56 and 72, and the ESD 74, which affect the capacity of the transmission 10 and the electric machines 56 and 72 to react input torque during the current loop cycle.

Inputs to the system constraints control path 360 include the immediate output torque request as measured by the accelerator pedal 113 (‘Output Torque Request Accel Immed’) and the immediate output torque request as measured by the brake pedal 112 (‘Output Torque Request Brake Immed’) which are combined and shaped with the axle torque response type through an immediate output torque shaping filter 362 to yield a net immediate output torque (‘To Net Immed’) and an immediate accelerator output torque (‘To Accel Immed’). The net immediate output torque and the immediate accelerator output torque are inputs to a constraints scheme (‘Output and Input Torque Constraints’) 364. Other inputs to the constraints scheme 364 include the lead operating range state of the transmission 10, an immediate lead input acceleration profile (‘Lead Input Acceleration Profile Immed’), a lead immediate clutch reactive torque range (‘Lead Immediate Clutch Reactive Torque Min/Max’) for each applied clutch in the lead operating range state A targeted lead input acceleration profile comprises a time-shifted lead of the immediate input acceleration profile of the input member 12 to accommodate a response time lag between a commanded change in the immediate input acceleration profile and a measured change in the immediate input acceleration profile. The lead immediate clutch reactive torque range comprises a time-shifted lead of the immediate clutch reactive torque range of the clutches to accommodate a response time lag between a commanded change in the immediate clutch torque range and a measured change in the immediate clutch reactive torque range. The constraints scheme 364 determines an output torque range for the transmission 10, and then determines the minimum and maximum input torques that can be reacted by the transmission 10 based upon the aforementioned inputs.

The minimum and maximum input torques are input to the engine torque conversion calculator 355 and converted to minimum and maximum engine torques (‘Engine Torque Hybrid Minimum’ and ‘Engine Torque Hybrid Maximum’ respectively), by taking into account parasitic and other loads introduced between the engine 14 and the transmission 10.

The filtered target engine torque, the output of the engine state machine 372 and the engine minimum and maximum engine torques are input to the engine response type determination scheme 380, which inputs the engine commands to the ECM 23 for controlling the engine state, the immediate engine torque request and the predicted engine torque request. The engine commands include an immediate engine torque request (‘Engine Torque Request Immed’) and a predicted engine torque request (‘Engine Torque Request Prdtd’) that can be determined based upon the filtered target engine torque. Other commands control the engine state to one of the engine in the fueled state and the deceleration fuel cutoff state (‘FCO Request’) and to one of the cylinder deactivation state and the all-cylinder state (‘DEAC Request’). Another output comprises an engine response type (‘Engine Response Type’). When the filtered target engine torque is within the range between the minimum and maximum engine torques, the engine response type is inactive. When the filtered target engine torque is outside the constraints of the minimum and maximum engine torques (‘Engine Torque Hybrid Minimum’) and (‘Engine Torque Hybrid Maximum’) the engine response type is active, indicating a need for an immediate change in the engine torque, e.g., through engine spark control and retard to change the engine torque and the input torque to fall within the constraints of the minimum and maximum engine torques.

FIG. 5 depicts the stabilization analysis scheme 356 including an engine transition cost function (‘Engine Transition Costs’) 510, an optimization stabilization cost function (‘Optimization Stabilization Costs’) 520, and an engine state determination function (‘Engine State Determination’) 530. Operation of the engine 14 is controlled to transfer torque to the input member 12. This includes monitoring the operator torque request and determining operating power costs associated with candidate engine states in response to the operator torque request. Transition costs for transitioning the engine 14 from a present engine state to each of the candidate engine states are determined. Stabilization costs for operating the engine 14 in the present engine state and subsequently operating the engine 14 in each of the candidate engine states can be determined. One of the candidate engine states is selected as a preferred engine state based upon the operating power costs, the transition costs, and the stabilization costs for the plurality of engine states. The operating power costs for operating the engine at one of the candidate engine states are based upon power costs to generate an input torque and associated operating power costs for operating the transmission 10 to generate an output torque that is responsive to the operator torque request. The operating power costs for operating the engine in the candidate engine state are based upon engine fuel consumption level at the generated input torque at the candidate engine state. There is an associated powertrain energy consumption that is determined based upon operating the hybrid transmission to generate the output torque responsive to the operator torque request and the input torque for the candidate engine state.

The engine transition cost function 510 monitors the present engine state (‘Actual Engine State’), and determines transition costs (‘P_(COST FULL FUEL2)’, ‘P_(COST FULL FCO2)’, ‘P_(COST DEAC FUEL2)’, ‘P_(COST DEAC FCO2)’) associated with transitioning between the present engine state and each candidate engine state (‘Potential Engine State’). The transition costs are based upon energy and power costs associated with an engine state transition wherein fuel or electric power is consumed during the transition without a corresponding increase in the output power or the output power can be reduced while input power from the engine 14 and the first and second electric machines 56 and 72 remains unchanged. Preferably the transition costs are predetermined and stored as a lookup table in one of the memory devices. The transition costs include a fuel cutoff, all-cylinder to fueled, all-cylinder transition cost (‘PCOST1 ’); a fueled, cylinder deactivation to fueled, all-cylinder transition cost (‘PCOST2’); a fuel cutoff, cylinder deactivation to fueled, all-cylinder transition cost (‘PCOST3’); a fueled, all-cylinder to fuel cutoff, all-cylinder transition cost (‘PCOST4’); a fueled, cylinder deactivation to fuel cutoff, all-cylinder transition cost (‘PCOST5’); a fuel cutoff, cylinder deactivation to fuel cutoff, all-cylinder transition cost (‘PCOST6’); a fueled, all-cylinder to fueled, cylinder deactivation transition cost (‘PCOST7’); a fuel cutoff, all-cylinder to fueled, cylinder deactivation transition cost (‘PCOST8’); a fuel cutoff, cylinder deactivation to fueled, cylinder deactivation transition cost (‘PCOST9’); a fueled, all-cylinder to fuel cutoff, cylinder deactivation transition cost (‘PCOST10’); a fuel cutoff, all-cylinder to fuel cutoff, cylinder deactivation transition cost (‘PCOST11’); and a fueled, cylinder deactivation to fuel cutoff, cylinder deactivation transition cost (‘PCOST12’). The transition costs are zero when the candidate engine state equals the present engine state.

The optimization stabilization cost function 520 monitors a previous preferred engine state, and determines stabilization costs (‘P_(COST FULL FUEL3)’, ‘P_(COST FULL FCO3)’, ‘P_(COST DEAC FUEL3)’, ‘P_(COST DEAC FCO3)’) for transitioning between a preferred engine state of the previous 25 ms loop cycle, which is accessed from one of the storage mediums, and each of the candidate engine states (‘Potential Engine State’). The optimization stabilization costs are based upon energy and power costs associated with the engine state transition, as previously described, and costs associated with driveability costs. Preferably the optimization stabilization costs are predetermined and stored as a lookup table in one of the memory devices. The optimization stabilization costs include a fuel cutoff, all-cylinder to fueled, all-cylinder stabilization cost (‘PCOST13’); a fueled, cylinder deactivation to fueled, all-cylinder stabilization cost (‘PCOST14’); a fuel cutoff, cylinder deactivation to fueled, all-cylinder stabilization cost (‘PCOST15’); a fueled, all-cylinder to fuel cutoff, all-cylinder stabilization cost (‘PCOST16’); a fueled, cylinder deactivation to fuel cutoff, all-cylinder stabilization cost (‘PCOST17’); a fuel cutoff, cylinder deactivation to fuel cutoff, all-cylinder stabilization cost (‘PCOST18’); a fueled, all-cylinder to fueled, cylinder deactivation stabilization cost (‘PCOST19’); a fuel cutoff, all-cylinder to fueled, cylinder deactivation stabilization cost (‘PCOST20’); a fuel cutoff, cylinder deactivation to fueled, cylinder deactivation stabilization cost (‘PCOST21’); a fueled, all-cylinder to fuel cutoff, cylinder deactivation stabilization cost (‘PCOST22’); a fuel cutoff, all-cylinder to fuel cutoff, cylinder deactivation stabilization cost (‘PCOST23’); and a fueled, cylinder deactivation to fuel cutoff, cylinder deactivation stabilization cost (‘PCOST24’). The optimization stabilization cost is zero when the candidate engine state equals the previous preferred engine state.

The engine state determination function 530 monitors the operating costs from the optimization scheme 354, the transition costs associated with the present engine state from the engine transition cost function 510, and the optimization stabilization costs associated with the previous preferred engine state from the optimization stabilization cost function 520 for each of the candidate engine states. The engine state determination function 530 monitors the enable signals that indicate which of the candidate engine states is available and therefore, whether a transition to the candidate engine state is allowed. The enablement signals include a fueled, cylinder deactivation enablement signal (‘Enable Deac Fuel’); a fuel cutoff, cylinder deactivation enablement signal (‘Enable Deac FCO’); and a fuel cutoff, all-cylinder enablement signal (‘Enable Full FCO’). The fueled, all-cylinder state is always enabled.

The engine state determination function 530 determines an overall operating cost for each of the candidate engine states by summing the operating costs from the optimization scheme 354, the transition costs associated with the present engine state from the engine transition cost function 510, and the optimization stabilization costs associated with the previous preferred engine state from the optimization stabilization cost function 520 for each candidate engine state. The engine state determination function 530 determines and outputs the preferred engine state (‘Preferred Engine State’) based on the lowest cost among the candidate engine states that are allowed based upon the enablement signals.

The stabilization analysis scheme 356 determines the preferred engine state based on operating costs indicating powertrain operating efficiency, thereby providing fuel efficient operation of the powertrain system. Further, the stabilization analysis scheme 356 determines the preferred engine state based upon the transition costs and optimization stabilization costs to avoid excessive transitioning between engine states and variations in engine torque requests, thereby improving fuel economy and reducing potential noise, vibration, and harshness concerns.

The disclosure has described certain preferred embodiments and modifications thereto. Further modifications and alterations may occur to others upon reading and understanding the specification. Therefore, it is intended that the disclosure not be limited to the particular embodiment(s) disclosed as the best mode contemplated for carrying out this disclosure, but that the disclosure will include all embodiments falling within the scope of the appended claims. 

1. Method for controlling an engine selectively operative in one of a plurality of engine states to transfer torque to an input member of a hybrid transmission, the hybrid transmission operative to transfer torque between the input member and a torque machine and an output member to generate an output torque in response to an operator torque request, the method comprising: monitoring the operator torque request; determining operating power costs associated with a plurality of candidate engine states in response to the operator torque request; determining transition costs for transitioning the engine from a present engine state to each of the candidate engine states; determining stabilization costs for operating the engine in the present engine state and subsequently operating the engine in each of the candidate engine states; and selecting a preferred engine state based upon the operating power costs, the transition costs, and the stabilization costs for the plurality of engine states.
 2. The method of claim 1, further comprising determining operating power costs for operating the engine at one of the candidate engine states to generate an input torque and determining associated operating power costs for operating the hybrid transmission to generate an output torque responsive to the operator torque request.
 3. The method of claim 2, comprising determining the operating power costs for operating the engine in the candidate engine state based upon engine fuel consumption level at the generated input torque at the candidate engine state and powertrain energy consumption associated with operating the hybrid transmission to generate the output torque responsive to the operator torque request.
 4. The method of claim 1, wherein selecting the preferred engine state comprises selecting the candidate engine state that minimizes a combination of the operating power costs, the transition costs, and the stabilization costs.
 5. The method of claim 1, further comprising transitioning the engine to operate at the preferred engine state.
 6. The method of claim 1, wherein the candidate engine state comprises one of a fueled, all-cylinder state, a fuel cutoff, all-cylinder state, a fueled, cylinder deactivation state and a fuel cutoff, cylinder deactivation state.
 7. Method for controlling an engine selectively operative in one of a plurality of engine states to transfer torque to an input member of a hybrid transmission, the hybrid transmission operative to transfer torque between the input member and first and second electric machines and an output member to transmit an output torque to a driveline responsive to an operator torque request, the method comprising: monitoring the operator torque request; determining powertrain operating power costs associated with a plurality of candidate engine states in response to the operator torque request; determining transition costs for transitioning the engine from a present engine state to each of the candidate engine states; determining stabilization costs for operating the engine in the present engine state and subsequently operating the engine in each of the candidate engine states; and selecting one of the candidate engine states based upon the operating power costs, the transition costs, and the stabilization costs for the plurality of engine states.
 8. The method of claim 7, further comprising determining operating power costs for operating the engine at one of the candidate engine states to generate an input torque and determining associated operating power costs for operating the first and second electric machines to transmit motor torque to the hybrid transmission to generate an output torque responsive to the operator torque request.
 9. The method of claim 8, comprising determining the operating power costs for operating the engine in the candidate engine state based upon engine fuel consumption level at the generated input torque at the candidate engine state and powertrain energy consumption for operating the hybrid transmission to generate the output torque responsive to the operator torque request.
 10. The method of claim 7, further comprising selecting the candidate engine state that minimizes a combination of the operating power costs, the transition costs, and the stabilization costs.
 11. The method of claim 7, further comprising transitioning the engine to operate at the preferred engine state.
 12. The method of claim 11, wherein the candidate engine state comprises one of a fueled, all-cylinder state, a fuel cutoff, all-cylinder state, a fueled, cylinder deactivation state and a fuel cutoff, cylinder deactivation state. 